Study of Non-Equilibrium Flow Behind Normal Shock

Study of Non-Equilibrium Flow Behind Normal Shock

Normal shock problems in high enthalpy flows are of special interests to aerodynamicists and fluid dynamicists. When the shock Mach number become hypersonic and increasing further, the gas passing through the shock is compressed resulting in increase in temperature and pressure. As the Mach number i...

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Bibliographic Details
Main Author: Malik, Bijoy Kumar
Other Authors: Ramesh, O N
Language:en_US
Published: 2017
Subjects:
Shock Waves
Supersonic Aerodynamics
Fluid Dynamics
Non-Equilibrium Flows
Unsteady Shock
An-harmonic Oscillator Theory
Diatomic Dissociation
Oscillator Model
Shock (Mechanics)
Ionization
Morse Oscillator Theory
Shock Flow
Aerospace Engineering
Online Access:http://etd.iisc.ernet.in/handle/2005/2891

Internet

http://etd.iisc.ernet.in/handle/2005/2891

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